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Anderson Greenwood AG-14

Light Utility · Cold War (1970–1991)

Anderson Greenwood AG-14 — Light Utility
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The Anderson Greenwood AG-14 is a two-seat utility aircraft developed in the United States shortly after World War II. It is an all-metal, shoulder-wing monoplane of pod-and-boom configuration, equipped with a pusher propeller, side-by-side seating and fixed tricycle undercarriage.

Specifications

Category
Fixed Wing
Sub-Category
Light Utility
Domain
Civil
Era
Cold War (1970–1991)
Engine
1× 4-cylinder air-cooled horizontally-opposed piston engine
Thrust / Power
90 hp
Length (ft)
22
Wingspan (ft)
34
Empty Weight (lb)
850
MTOW (lb)
1400
Service Ceiling (ft)
16500
Max Speed (mph)
120